Piston cooling for opposed-piston engine

ABSTRACT

Pistons for opposed-piston engines include an interior annular cooling gallery. The gallery is provided with inlet and drain passageways constructed to shield a jet of liquid coolant entering the gallery, thereby reducing interference between the incoming jet and liquid coolant circulating in the gallery.

PRIORITY

This application is a continuation of U.S. application Ser. No.14/596,855, filed on Jan. 14, 2015 for “Piston Cooling ForOpposed-Piston Engines”, which will issue as U.S. Pat. No. 9,759,119 onSep. 12, 2017.

RELATED APPLICATIONS

This application contains subject matter related to the subject matterof the following commonly-owned U.S. patent application Ser. No.13/136,955, filed Aug. 15, 2011 for “Piston Constructions forOpposed-Piston Engines,” published as US 2012/0073526 on Mar. 29, 2012;Ser. No. 13/776,656, filed Feb. 25, 2013 for “Rocking Journal Bearingsfor Two-Stroke Cycle Engines,” published as US 2014/0238360 on Aug. 28,2014; Ser. No. 14/075,926, filed Nov. 22, 2013 for “LubricatingConfiguration For Maintaining Wristpin Oil Pressure In A Two-StrokeCycle, Opposed-Piston Engine;” and, Ser. No. 14/199,877, filed Mar. 6,2014 for “Piston Cooling Configuration Utilizing Lubricating Oil From ABearing Reservoir In An Opposed-Piston Engine.”

TECHNICAL FIELD

The technical field of this disclosure includes internal combustionengines, particularly two-stroke, opposed-piston engines. In one aspect,the technical field relates to cooling the pistons of opposed-pistonengines.

BACKGROUND

The related patent applications describe two-stroke, opposed-pistonengines in which pairs of pistons move in opposition to form shapedcombustion chambers between their end surfaces. During a compressionstroke, two opposed pistons move toward each other in the direction ofrespective top center locations in the bore of a ported cylinder. As thepistons near the top center locations, charge air is compressed betweentheir end surfaces and fuel is injected through the side of the cylinderinto the combustion chamber formed by the end surfaces. The heat of thecompressed air ignites the fuel and combustion occurs. In response tocombustion, the pistons reverse direction in a power stroke. During thepower stroke, the pistons move away from each other toward bottom centerlocations in the bore. As the pistons reciprocate between top and bottomcenter locations they open and close ports formed in respective intakeand exhaust locations of the cylinder in timed sequences that controlthe flow of charge air into, and exhaust from, the cylinder.

In some aspects of piston constructions for two-stroke, opposed-pistonengines it is desirable to utilize pistons with crowns having contouredend surfaces that interact with swirl and with squish flow from theperiphery of the combustion chamber to produce complex, turbulent chargeair motion that encourages mixing of air and fuel. However, combustionimposes a heavy thermal load on the piston crowns. The contoured endsurfaces create non-uniform thermal profiles that are not suitablycooled by conventional forced cooling configurations, leading toasymmetrical thermal stress, wear, and piston crown fracture. In orderto increase piston durability and to contribute to effective thermalmanagement of the engine, it is therefore desirable to provide pistonconstructions with the capability of cooling the contoured crowns ofsuch pistons.

In some instances, a piston cooling construction for opposed pistonsincludes an internal annular cooling gallery in each piston throughwhich a liquid coolant (for example, lubricating oil) circulates. Seethe related, commonly-owned U.S. patent application Ser. No. 13/136,955,published as US 2012/0073526, in this regard. The annular galleryfollows the piston's periphery along the under surface of the crown; itis closed except for one or more openings and one or more slots in thegallery floor that respectively admit liquid coolant into and drainliquid coolant from the annular gallery. The dimension of the gallery inthe longitudinal dimension of the piston (the height of the gallery)varies between a maximum where the gallery abuts a protruding ridge onthe crown end surface and a minimum where the gallery abuts a notch onthe end surface through which fuel is injected into the combustionchamber. An opening in the gallery floor provides entry for a jet ofliquid coolant transmitted through an open end of the piston skirt. Insome instances, these openings are located so as to allow the jets ofliquid coolant to strike a portion of the crown under surface lyingabutting a ridge on the end surface because the ridge bears a heavythermal load during engine operation. In some instances, liquid coolantis drained from the annular gallery at about the same level at which thejet enters the gallery. Drained liquid coolant flows into the interiorof the piston skirt and then out the open end.

Taking into account oscillation of each of the opposed pistons duringhigh speed operation of the engine and suboptimal drainage through thecentral gallery, liquid coolant can collect and dwell in a creasedportion of an annular gallery under a ridge, creating a standing body ofliquid coolant. If a jet is aimed at this portion the standing body ofliquid coolant can attenuate the impingement effects of the jet andimpair circulation of the liquid within the gallery.

It is desirable for liquid coolant to enter the annular galleryunimpeded and to reach and flow across the crown under surface so as toensure effective cooling. Further, it is desirable for the liquidcoolant to drain unimpeded from the gallery. However, when coolantenters and drains at the same level in the gallery, accumulated coolantin the gallery can disrupt an incoming jet and conversely, an incomingjet can disrupt the coolant moving in the gallery. Either or both ofthese effects can result in suboptimal circulation through the galleryand muted cooling performance.

It is therefore desirable to improve circulation of liquid coolant inthe piston cooling gallery by protecting the incoming jet and reducingor eliminating interference between incoming and effluent streams ofliquid coolant in the gallery.

SUMMARY

An objective of the piston cooling gallery described in this disclosureis to protect or shield an incoming liquid coolant jet from coolantalready present in the gallery. A further objective is to separate andposition inlet and drain passageways in the piston cooling gallery insuch a way as to improve the circulation of liquid coolant therethrough.

Preferably, a cooling gallery construction for pistons of opposed-pistonengines includes separate inlet and drain passageways with respectiveopenings at differing distances from the crown under surface. In someaspects, the outlet opening of an inlet passageway through which anincoming jet of coolant enters the cooling gallery is closer to thecrown under surface than the drain opening of a drain passageway.

In further aspects, the difference in distance is due, at least in part,to placement of the drain opening of the drain passageway in abowl-shaped depression in the cooling gallery.

In other aspects, the inlet passageway extends out of the bowl-shapeddepression in the direction of the crown under surface.

In still other aspects, the inlet passageway is positioned so as to aima jet of liquid coolant at a portion of the crown under surface having aconvex shape.

A piston for an opposed-piston engine constructed according to thisdisclosure has a longitudinal axis, a crown, and a skirt part with apiston sidewall. The crown has an end surface shaped to define acombustion chamber with the end surface of an opposing piston in theengine. The piston sidewall extends along the longitudinal axis from thecrown to an open end of the skirt. An annular cooling gallery within thepiston is defined between an interior wall of the skirt and an undersurface of the crown. At least one coolant inlet passageway in theinterior wall includes an outlet opening in the cooling gallery fromwhich a jet of liquid coolant emerges into the gallery. At least onecoolant drain passageway in the interior wall includes a drain openingin the cooling gallery. The outlet opening is positioned a firstdistance from the crown under surface, and the drain opening ispositioned at a second distance from the crown under surface which isgreater than the first distance.

In some aspects, the drain opening is located in a bowl in the interiorwall that faces the crown under surface. In some further aspects, thedrain passageway and the inlet passageway extend along a longitudinalportion of the piston sidewall that runs between indented portions ofthe piston sidewall.

In an embodiment of the piston, the piston sidewall includeslongitudinal skirt portions running from the crown to the open end thatare separated from one another by intervening sidewall indentationsrunning between the crown and the open end. An interior wall of theskirt within the sidewall includes a wristpin bore that extends betweenopposing sidewall indentations. An annular cooling gallery within thepiston is defined between the interior wall and an under surface of thecrown. At least one coolant inlet passageway having an outlet opening inthe cooling gallery and at least one coolant drain passageway having adrain opening in the cooling gallery are formed in the interior wall inthe vicinity of a longitudinal skirt portion. The outlet opening ispositioned a first distance from a convex portion of the crown undersurface, and the drain opening is positioned at a second distance fromthe convex portion of the crown under surface which is greater than thefirst distance.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an isometric view of a piston constructed for use in anopposed-piston engine, in which piston cooling aspects and embodimentsaccording to this disclosure are incorporated.

FIG. 2 is an exploded view of the piston of FIG. 1.

FIG. 3A is a side sectional view of the piston of FIG. 1 through a planethat includes the longitudinal axis of the piston and the axis of awristpin. FIG. 3B is a side sectional view of the piston of FIG. 1through a plane that includes the longitudinal axis of the piston and isorthogonal to the axis of the wristpin.

FIG. 4 is a conceptual schematic representation of piston coolingaccording to this disclosure.

FIG. 5 is an isometric view into a skirt part of the piston of FIG. 1,showing inet and drain openings in the cooling gallery.

FIG. 6 is a view along the longitudinal axis of the piston of FIG. 1into an open end of the skirt part of FIG. 1.

FIG. 7 is a side sectional view of the piston of FIG. 1 through a planethat corresponds to the sight lines A-A in FIG.

FIG. 8 illustrates an alternative inlet passageway embodiment.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

In this description, the term “jet” is intended to refer to a forcefulstream or flow of liquid coolant discharged from a narrow opening. Inthe relevant arts, “jet” may also refer to a nozzle or tube throughwhich the forceful stream or flow of liquid coolant is delivered foruse. In this latter regard, we have chosen, for clarity's sake, to usethe term “nozzle” so as to avoid confusing the stream from its channel,without intending to exclude other terms that are synonymous withnozzle, including “jet”.

FIG. 1 illustrates an example of a piston 10 for an opposed-pistonengine constructed according to this disclosure. The piston 10 has alongitudinal axis 12, a crown 14, and a skirt part 16 with a pistonsidewall 18. The piston sidewall 18 is generally cylindrical and extendsalong the longitudinal axis 12. The crown 14 has an end surface 20shaped to define a combustion chamber with the end surface of anopposing piston in the engine. The shape of the end surface 20 shown inFIG. 1 limits the scope of this disclosure only to the extent that itcooperates with the end surface of an opposing piston to define a shapeof a combustion chamber in an opposed-piston engine. Many other such endsurface shapes are possible; see, for example, and without limitation,the end surface shapes for pistons of opposed-piston engines that aredescribed and illustrated in US 2013/0213342 A1, US 2014/0014063 A1, US2014/0083396 A1, and U.S. Pat. No. 8,800,528 B2.

With reference to FIGS. 2, 3A and 38, the sidewall 18 runs from a firstend 21 (see also FIG. 5) to a second end 22 (see also FIG. 6) of theskirt part 18. As best seen in FIGS. 3A, 3B, and 6, the second end isopen. An interior wall 23 of the skirt that is centered on thelongitudinal axis 12 is situated in the sidewall near the first end 21.In some aspects, the interior wall 23 includes support structures for awristpin and a cooling chamber. Preferably, but not necessarily, theinterior wall 23 on one side (seen in FIG. 6) defines a portion of awristpin bore 24 where a wristpin is received and retained. The wristpinmay comprise, for example and without limitation, a biaxial bearing unitas described and illustrated in US 2014/0238360 A1. In this regard, abearing sleeve 26 is received in the wristpin bore 24 where it supportsa wristpin journal 28 against the one side of the interior wall 23 foroscillatory rocking during engine operation. Discs 30 retain the sleeve26 and journal 28 in the wristpin bore 24. Preferably, the interior wall23 on the opposite side (seen in FIG. 5) defines a portion of an annularcooling gallery 32. As per FIGS. 3A and 3B, the interior wall 23includes a structural base for the annular cooling gallery 32 within thepiston 10. The gallery 32 is defined between an outer peripheral section34 of the interior wall 23 and an outer peripheral portion of the undersurface 36 of the crown 14. The annular cooling gallery 32 is closedexcept for inlet and drain passageways 38 and 42 in the interior wall 23(best seen in FIGS. 5 and 6).

The materials and methods of construction of the piston 10 areconventional for medium and/or heavy duty use or for large boreapplications. For example, the crown and skirt part may be formedseparately of compatible materials (e.g., forged steel crown, cast ironskirt part) and joined by welding or brazing.

FIG. 4 is a conceptual schematic cross-section of a portion of thecooling gallery 32 that represents principles of piston coolingaccording to this disclosure. In this regard, at least one coolant inletpassageway 38 running in the interior wall 23 includes an outlet opening40 in the cooling gallery 32. At least one coolant drain passageway 42in the interior wall 23 includes a drain opening 44 in the coolinggallery 32. The coolant outlet opening 40 is positioned in a referenceplane 46 that divides the cooling gallery into first and second portionsand is orthogonal to the longitudinal axis 12. The drain opening 44 ispositioned at a distance from the reference plane 46 in the direction ofthe open end 22 of the skirt. From this aspect, the outlet opening 40 isnearer the crown under surface 36 than the drain opening. From anotheraspect, the coolant outlet and drain openings 40 and 44 are separatedwithin the piston by a longitudinal distance D, with the coolant drainopening 44 being nearer to the open end of the skirt than the coolantoutlet opening 40. From yet another aspect, the outlet opening 40 ispositioned a first distance D₁ from the under surface 36 of the crown14, each drain opening 44 is positioned a second distance D₂=(D+D₁) fromthe under surface of the crown, and the second distance is greater thanthe first distance (D₂>D₁). From any point of view, an infusing jet 52of liquid coolant transmitted from a dedicated nozzle 54 aimed at anopen end of the piston skirt travels through the inlet passageway 38 andenters the cooling gallery 32 through the outlet opening 40 at a levelnearer the crown under surface 36 than the level from which the coolantis drained through the drain openings 44. The arrangement of the outletand drain openings 40 and 44 at these different levels separates andreduces interference between the infusing jet 52 and liquid coolant inthe cooling gallery 32, including an effusing flow of liquid that passesthrough the drain opening 44 and travels within the skirt part 16 towardand through the open end 22. From another aspect, the separation of theinlet and drain passageways, and the placement of the outlet and drainopenings at different levels of the annular cooling gallery 32 shieldsthe jet 52 from liquid coolant circulating in the cooling gallery.

In some aspects, the outlet opening 40 is positioned in alignment with aconvex portion 58 of the under surface 36. In these cases, the jet 52 ofliquid coolant spreads when it strikes the under surface 36 and avoidscollection increases that may be found in some embodiments of the undersurface 36. In some other aspects, there are two coolant drainpassageways 42 with respective drain openings 44 positioned at thedistance D from the reference plane 46. The drain openings 44 flank theinlet passageway 38 on either side, thereby flushing liquid coolant fromthe cooling gallery on either side of the outlet opening.

A preferred embodiment of the skirt part 16 showing an example ofconstruction of the interior wall 23 near the first end 21 the skirtpart 16 is seen from the point of view of the crown under surface inFIG. 5 and is seen through the open end 22 of the skirt part in FIG. 6.In this preferred embodiment, there are two coolant inlet passageways 38on opposite sides of the cooling gallery 32. Preferably, the inletpassageways 38 extend through the interior wall 23 and includerespective chimneys (or pipes, or tubes) 60 in the cooling gallery 32that extend in the direction of the crown under surface. Preferably, butnot necessarily, the inlet passageways have the oblong shape of astretched circle. In this embodiment, the outlet openings 40 are in theends of the chimneys 60. Two drain passageways 42 that flank each inletpassageway 38 extend through the interior wall 23. Each drain passagewayis positioned at the bottom of a respective bowl 62 formed in theinterior wall 23. Advantageously, the bowl and chimney configurationaffords a desirably substantial distance D separating an outlet opening40 from either or both of its flanking drain openings 44. Preferably,but not necessarily, the inlet passageways have oblong shapes incross-section, as would be formed by a stretched circle, per the planview of FIG. 6. Preferably, but not necessarily, the drain passagewayshave circular shapes in cross-section per the plan view of FIG. 6.

A representative embodiment of the piston 10 with cooling according tothis disclosure is shown in FIGS. 1, 3A, 3B, and 7. As per thesefigures, the outer peripheral surface of the crown 14 is formed with afirst set of ring grooves 64. A second set of ring grooves 66 is formedin a portion of the sidewall 18 near the open end 22 of the skirt. Inthis embodiment, the sidewall 18 is formed with opposing sidewallportions 68 separated from one another by intervening sidewallindentations 70. For example, there are two opposing side wall sections68 and two opposing indentations 70. The indentations 70 minimize boththe mass of the piston and contact area of the sidewall felt by the boreof a cylinder in which the piston is disposed. The sidewall portions 68extend from the crown 14 to the open end 22 of the skirt. Relative tothe longitudinal axis 12, the portions 68 of the sidewall have the sameradius as the crown 14 and the circumferential portion of the sidewallwhere the second set of ring grooves 66 is situated. The indentations 70run longitudinally in the sidewall 18 between the first ring grooves 64and the second ring grooves 66. As best seen in FIG. 6, there are inletpassageways 38 on opposite sides of the wristpin bore 24. Each inletpassageway 38 is positioned adjacent to (or, abuts) a respectivesidewall portion 68, where it is flanked on each side by a respectiveone of two drain passageways 42.

As per FIGS. 5 and 6, the inlet and drain passageways may be formedintegrally with the interior wall 23 by casting, forging, and/ormachining the skirt part. Alternatively, as per FIG. 8, inletpassageways 38 may be constructed separately and then pressed, sintered,or welded into place in the interior wall 23. It may be advantageous insome applications to extend the inlet opening 72 of the inlet passagewaybeyond the outlet opening 74 of the drain passageway so that each jet 52of liquid coolant enters the inlet passageway 38 at a point nearer theopen end 22 of the skirt than the outlet opening 74 of the drainpassageway, thereby extending the shielding effect of the inletpassageway beyond the cooling gallery 32.

FIGS. 4 and 7 illustrate a method of cooling a piston 10 that has acrown 14 with an end surface 20 shaped to define a combustion chamberwith an end surface of an opposing piston in an opposed-piston engine, askirt part 16 joined to the crown, and an annular cooling gallery 32within the piston defined between the crown and the skirt part. Themethod includes providing at least one jet 52 of liquid coolant aimed ata convex portion 58 of the under surface 36 of the crown from a firstlevel 46 in the annular cooling gallery 32, and draining the liquidcoolant from a second level 47 in the annular gallery 32 that is furtherfrom the under surface 36 than the first level. In some aspects,draining the liquid coolant from the second level includes draining theliquid coolant at respective sides of the inlet passageway 38 throughwhich the jet travels into the annular gallery 32. In further aspects,the method includes providing respective jets of liquid coolant inopposite sides of the annular gallery 32.

Viewed alternatively, FIGS. 4 and 7 illustrate another method of coolinga piston that has a crown with an end surface shaped to define acombustion chamber with an end surface of an opposing piston in theopposed-piston engine, a skirt part joined to the crown, and an annularcooling gallery within the piston defined between the crown and theskirt part. This method includes providing at least one jet 52 of liquidcoolant aimed at an under surface 36 of the crown from an outlet 40 inthe annular cooling gallery, and shielding the jet 52 of liquid coolantfrom liquid coolant circulating in the annular gallery.

Although piston cooling according to this disclosure has been describedwith reference to specific examples and embodiments, it should beunderstood that various modifications can be made without departing fromthe spirit of the underlying principles. Accordingly, the scope ofinvention to be accorded hereto is limited only by the following claims.

1. A piston for an opposed-piston engine, comprising: a crown with anend surface shaped to define a combustion chamber with an end surface ofan opposing piston in an opposed-piston engine; a skirt part joined tothe crown and including a piston sidewall extending from the crown to anopen end of the skirt part; an annular cooling gallery defined betweenthe crown and the skirt part; a first set of ring grooves formed in anouter peripheral surface of the crown; a second set of ring groovesformed in formed in a portion of the sidewall near the open end of theskirt; the sidewall comprising two opposing sidewall portions separatedfrom one another by two intervening sidewall indentations; and, awristpin bore extending between the sidewall indentations.
 2. The pistonof claim 1, wherein the sidewall portions extend from the crown to theopen end of the skirt, and the indentations run longitudinally in thesidewall between the first ring grooves and the second ring grooves. 3.The piston of claim 1, in which the skirt part has an interior wall neara first end of the sidewall and the annular cooling gallery is definedbetween a first side of the interior wall and an under surface of thecrown.
 4. The piston of claim 3, in which a second side of the interiorwall opposite the first side includes at least a portion of a wristpinbore.
 5. The piston of any one of claims 1-4, comprising a wristpinreceived in the wristpin bore.
 6. The piston of claim 5, in which thewristpin comprises a biaxial bearing unit.
 7. The piston of claim 6, inwhich the biaxial bearing unit comprises a bearing sleeve received inthe wristpin bore and a wristpin journal supported by the bearing sleevefor oscillatory rocking during operation of the opposed-piston engine.8. A piston for an opposed-piston engine, the piston having alongitudinal axis and comprising: a crown with an end surface shaped todefine a combustion chamber with an end surface of an opposing piston inan opposed-piston engine; a skirt part joined to the crown; the crownincluding first ring grooves; the skirt part including second ringgrooves spaced apart from the first ring grooves along the longitudinalaxis; the skirt part including a piston sidewall with opposing skirtportions extending from the first to the second ring grooves andseparated from one another by intervening sidewall indentations runningalong the longitudinal axis between the first and second ring grooves;an annular cooling gallery within the piston; a wristpin bore extendingbetween the sidewall indentations.
 9. The piston of claim 8, wherein thesidewall portions extend from the crown to an open end of the skirt. 10.The piston of claim 8, in which the skirt part has an interior wall neara first end of the sidewall and the annular cooling gallery is definedbetween a first side of the interior wall and an under surface of thecrown.
 11. The piston of claim 10, in which a second side of theinterior wall opposite the first side includes at least a portion of awristpin bore.
 12. The piston of any one of claims 8-11, comprising awristpin received in the wristpin bore.
 13. The piston of claim 12, inwhich the wristpin comprises a biaxial bearing unit.
 14. The piston ofclaim 13, in which the biaxial bearing unit comprises a bearing sleevereceived in the wristpin bore and a wristpin journal supported by thebearing sleeve for oscillatory rocking during operation of theopposed-piston engine.